RU2654270C2 - Соединение для композитных крыльев - Google Patents

Соединение для композитных крыльев Download PDF

Info

Publication number
RU2654270C2
RU2654270C2 RU2013150275A RU2013150275A RU2654270C2 RU 2654270 C2 RU2654270 C2 RU 2654270C2 RU 2013150275 A RU2013150275 A RU 2013150275A RU 2013150275 A RU2013150275 A RU 2013150275A RU 2654270 C2 RU2654270 C2 RU 2654270C2
Authority
RU
Russia
Prior art keywords
wing
stringer
shaped
far
noodle
Prior art date
Application number
RU2013150275A
Other languages
English (en)
Russian (ru)
Other versions
RU2013150275A (ru
Inventor
Чан-Лианг ЛИН
Райан М. МАН
Карл Б. ЛИ
Original Assignee
Зе Боинг Компани
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Зе Боинг Компани filed Critical Зе Боинг Компани
Publication of RU2013150275A publication Critical patent/RU2013150275A/ru
Application granted granted Critical
Publication of RU2654270C2 publication Critical patent/RU2654270C2/ru

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/26Construction, shape, or attachment of separate skins, e.g. panels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26Attaching the wing or tail units or stabilising surfaces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/182Stringers, longerons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/185Spars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49616Structural member making
    • Y10T29/49622Vehicular structural member making

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Plates (AREA)
  • Slide Fasteners, Snap Fasteners, And Hook Fasteners (AREA)
  • Packages (AREA)
  • Clamps And Clips (AREA)
RU2013150275A 2012-11-13 2013-11-12 Соединение для композитных крыльев RU2654270C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/675,809 2012-11-13
US13/675,809 US9272769B2 (en) 2012-11-13 2012-11-13 Joint for composite wings

Publications (2)

Publication Number Publication Date
RU2013150275A RU2013150275A (ru) 2015-05-20
RU2654270C2 true RU2654270C2 (ru) 2018-05-17

Family

ID=49683419

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2013150275A RU2654270C2 (ru) 2012-11-13 2013-11-12 Соединение для композитных крыльев

Country Status (9)

Country Link
US (1) US9272769B2 (ko)
EP (1) EP2730498B1 (ko)
JP (1) JP5808379B2 (ko)
KR (2) KR20140061237A (ko)
CN (1) CN103803054B (ko)
AU (1) AU2013245438B2 (ko)
BR (1) BR102013029090B1 (ko)
ES (1) ES2738790T3 (ko)
RU (1) RU2654270C2 (ko)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9580164B2 (en) * 2013-07-10 2017-02-28 The Boeing Company Apparatus and methods for joining aircraft composite structures
RU2613661C1 (ru) * 2016-01-11 2017-03-21 Федеральное государственное бюджетное образовательное учреждение высшего образования Казанский национальный исследовательский технический университет им. А.Н. Туполева-КАИ" (КНИТУ-КАИ) Способ сборки крыла из полимерного композиционного материала
US10329008B2 (en) * 2016-06-24 2019-06-25 The Boeing Company Fluid-tight mechanical fastening system and associated structural assembly
US10696373B2 (en) 2016-09-13 2020-06-30 The Boeing Company Aircraft wings and aircraft including such aircraft wings
US9964131B1 (en) * 2017-04-28 2018-05-08 The Boeing Company Methods and apparatuses for providing corrosion protection to joined surfaces
US10766598B2 (en) 2017-06-14 2020-09-08 The Boeing Company Wing-to-fuselage joints and aircraft including the same
US10773787B2 (en) 2017-06-14 2020-09-15 The Boeing Company Wing-to-fuselage joints and aircraft including the same
IL259149B (en) 2018-05-03 2022-09-01 Israel Aerospace Ind Ltd Structural elements made of composite materials
US11433990B2 (en) * 2018-07-09 2022-09-06 Rohr, Inc. Active laminar flow control system with composite panel
US10786955B2 (en) 2018-07-16 2020-09-29 The Boeing Company Apparatuses and methods for fabricating a composite structure and reacting to a placement force
US11230072B2 (en) 2018-07-16 2022-01-25 The Boeing Company Apparatuses for fabricating a composite structure and reacting to a placement force
CN109114079A (zh) * 2018-09-21 2019-01-01 中国五冶集团有限公司 一种钢板结构的连接机构
CN109592002B (zh) * 2018-11-02 2022-03-15 中国航空工业集团公司西安飞机设计研究所 一种飞机复合材料壁板对接方法
FR3092269A1 (fr) 2019-02-04 2020-08-07 Airbus Operations Procédé de fabrication à partir de préformes d’éléments de liaison d’une aile d’aéronef à un caisson central de voilure
CN110027696A (zh) * 2019-04-30 2019-07-19 中国商用飞机有限责任公司 飞机下壁板的对接结构
US11198497B2 (en) * 2019-06-19 2021-12-14 The Boeing Company Splice fittings that are affixed to stringers via web-installed fasteners
CN110406657B (zh) * 2019-07-31 2021-06-01 中国商用飞机有限责任公司北京民用飞机技术研究中心 民用飞机机翼上壁板根部连接角盒、连接结构及机翼
CN110498036B (zh) * 2019-08-07 2021-08-17 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种尾翼壁板连接结构、尾翼和飞机
WO2021157672A1 (en) * 2020-02-04 2021-08-12 Hapsmobile Inc. Trailing edge spar connection for an unmanned aerial vehicle
CN111392028A (zh) * 2020-04-13 2020-07-10 中国商用飞机有限责任公司 用于机翼长桁的长桁修理件以及修理机翼长桁的方法
CN112591073B (zh) * 2020-12-23 2021-09-24 北京北航天宇长鹰无人机科技有限公司 一种翼身结合接头及无人机
CN113664530B (zh) * 2021-09-06 2022-09-13 上海航天精密机械研究所 一种助推尾段型架尾翼对接接头的定位装置及装配方法

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2428352C1 (ru) * 2010-02-16 2011-09-10 ООО "Прогресстех" Устройство соединения панелей крыла и центроплана
US8573539B2 (en) * 2010-03-25 2013-11-05 Airbus Operations, S.L. Structure for joining torsion boxes in an aircraft using a triform fitting made from non-metallic composite materials

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4606961A (en) * 1984-10-09 1986-08-19 The Boeing Company Discretely stiffened composite panel
US5348602A (en) 1993-06-08 1994-09-20 General Electric Company Method for making a bonded laminated article bend portion
US5538589A (en) 1994-08-31 1996-07-23 The Boeing Company Composite stringer assembly machine
US6513757B1 (en) 1999-07-19 2003-02-04 Fuji Jukogyo Kabushiki Kaisha Wing of composite material and method of fabricating the same
DE60011286T2 (de) * 1999-11-15 2005-07-14 Therasense, Inc., Alameda Übergangsmetall-komplexverbindungen mit einer bidentaten ligande mit einem imidazol-ring
WO2001062495A2 (en) 2000-02-25 2001-08-30 The Boeing Company Laminated composite radius filler
FR2863324B1 (fr) * 2003-12-04 2007-12-14 Airbus France Procede de realisation d'une structure stratifiee et avion muni d'une telle structure
FR2873347B1 (fr) 2004-07-22 2006-11-17 Airbus France Sas Dispositif d'eclissage d'elements de structure composite avec des elements de structure metallique
US7303374B2 (en) 2005-03-08 2007-12-04 The Boeing Company Disbond resistant composite joint and method of forming
FR2883548B1 (fr) * 2005-03-23 2007-06-15 Airbus France Sas Dispositif et procede d'eclissage mixte carbone-metal dissymetrique
US7837148B2 (en) 2006-06-13 2010-11-23 The Boeing Company Composite wing-body joint
DE102007019692B4 (de) 2007-04-26 2011-06-01 Airbus Operations Gmbh Flügel-Rumpf-Sektion eines Flugzeugs
GB0708333D0 (en) 2007-04-30 2007-06-06 Airbus Uk Ltd Composite structure
GB0901228D0 (en) * 2009-01-26 2009-03-11 Airbus Uk Ltd Aircraft joint
GB0912015D0 (en) * 2009-07-10 2009-08-19 Airbus Operations Ltd Stringer
FR2948099B1 (fr) * 2009-07-16 2012-05-11 Airbus Operations Sas Procede de fabrication d'un aeronef a voilure fixe
ES2392236B1 (es) 2010-01-15 2013-10-09 Airbus Operations, S.L. Componente de aeronave con paneles rigidizados con larguerillos.
FR2957795B1 (fr) 2010-03-25 2012-06-15 Oreal Procede de coloration mettant en jeu un derive d'iridoide glycosyle
US8408493B2 (en) 2010-05-19 2013-04-02 The Boeing Company Composite stringer end trim
ES2396327B1 (es) 2010-06-10 2014-02-06 Airbus Operations, S.L. Procedimiento para la fabricación de piezas grandes de material compuesto controlando el espesor de sus bordes
GB201009922D0 (en) 2010-06-14 2010-07-21 Airbus Uk Ltd Aircraft wing box joint
US8578609B2 (en) 2010-10-27 2013-11-12 Airbus Operations S.L. Manufacturing procedure of a part made out of a composite material introducing a geometric change in one of its faces
US8974886B2 (en) * 2012-04-25 2015-03-10 The Boeing Company Disbond resistant composite stiffener runout

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2428352C1 (ru) * 2010-02-16 2011-09-10 ООО "Прогресстех" Устройство соединения панелей крыла и центроплана
US8573539B2 (en) * 2010-03-25 2013-11-05 Airbus Operations, S.L. Structure for joining torsion boxes in an aircraft using a triform fitting made from non-metallic composite materials

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
NIU, MICHAEL C.Y., COMPOSITE AIRFRAME STRUCTURES - PRACTICAL DESIGN INFORMATION AND DATA (3 Edition), AD ADASO/ADASTRA ENGINEERING LLC, 1992, pp. 327-348. *

Also Published As

Publication number Publication date
KR101790439B1 (ko) 2017-10-25
AU2013245438A1 (en) 2014-05-29
US9272769B2 (en) 2016-03-01
CN103803054B (zh) 2016-06-15
EP2730498A3 (en) 2017-11-15
KR20140061237A (ko) 2014-05-21
AU2013245438B2 (en) 2016-01-21
US20140131518A1 (en) 2014-05-15
CN103803054A (zh) 2014-05-21
JP2014097786A (ja) 2014-05-29
KR20160058732A (ko) 2016-05-25
ES2738790T3 (es) 2020-01-27
EP2730498A2 (en) 2014-05-14
JP5808379B2 (ja) 2015-11-10
BR102013029090B1 (pt) 2022-01-18
BR102013029090A2 (pt) 2014-10-21
EP2730498B1 (en) 2019-05-01
RU2013150275A (ru) 2015-05-20

Similar Documents

Publication Publication Date Title
RU2654270C2 (ru) Соединение для композитных крыльев
US11084269B2 (en) Multi-layer metallic structure and composite-to-metal joint methods
RU2636494C2 (ru) Композитные радиусные заполнители и способы их изготовления
CA2834721C (en) Stacked noodle for high capacity pull-off for a composite stringer
US8763253B2 (en) Vertical laminate noodle for high capacity pull-off for a composite stringer
US10308345B2 (en) Structure
US8939406B2 (en) Joining composite fuselage sections along window belts
KR20150034827A (ko) 접착식 복합 에어포일 및 이의 제작 방법
CA2783109C (en) Vertical laminate noodle for high capacity pull-off for a composite stringer
BR112013003588B1 (pt) Estrutura para aeronave composta híbrida de metal e resina e método de fabricação de uma estrutura composta
CA2829899C (en) Joint for composite wings
EP2650120B1 (en) Multi-layer metallic structure
CA2985314A1 (en) Carbon fiber reinforced polymer cargo beam with integrated cargo stanchions and c-splices

Legal Events

Date Code Title Description
HZ9A Changing address for correspondence with an applicant